Curtiss Condor
Technical Specifications
| First Flight: |
January 30, 1933 |
| Number Built: |
45 for commercial service |
| Length: |
48 feet 7 inches |
| Wing Span: |
82 feet |
| Height: |
N/A |
| Max Take-Off Wt.: |
17,500 lbs |
| Max Landing Wt.: |
N/A |
| Empty Wt.: |
N/A |
| Max Cruising Speed: |
N/A |
| Normal Cruising Speed: |
167 mph 145 kts |
| Stall Speed: |
N/A |
| Service Ceiling: |
23,000 feet |
| Fuel Capacity: |
N/A |
| Range: |
716 miles |
| Fuel Type: |
Octane |
| Fuel Consumption: |
N/A |
| Engines: |
2 Wright Cyclone SGR-1820-F3 Radial Engines |
| Seating: |
15 Passengers |
| Crew: |
2 Pilots 1 Flight Attendent |
Engine Specifications
Wright Cyclone SGR-1820-F3
|
| Type: |
9 cylinder air cooled radial |
| Length: |
N/A |
| Diameter: |
N/A |
| Bore: |
N/A |
| Stroke: |
N/A |
| Displacement: |
1820 cu. inches |
| Compression Ratio: |
N/A |
| Dry Weight: |
N/A |
| Ignition: |
N/A |
| Fuel Grade: |
Octane |
| Carburation: |
N/A |
| Performance: |
Rated @ 710 hp each @ take-off |
|